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1. 发明申请

US20110146284A1 Plate-like-object manufacturing method, plate-like objects, gas-turbine combustor, and gas turbine 有权
标题翻译：板状物体制造方法，板状物体，燃气轮机燃烧器和燃气轮机
公开(公告)号：US20110146284A1
公开(公告)日：2011-06-23
申请号：US12646115
申请日：2009-12-23
申请人： Hitoshi Morimoto , Hidenori Kanki , Tatsuo Ishiguro , Hiroki Shibata , Tetsu Konishi , Kenji Sato
发明人： Hitoshi Morimoto , Hidenori Kanki , Tatsuo Ishiguro , Hiroki Shibata , Tetsu Konishi , Kenji Sato
IPC分类号： F02C3/00 , B23P19/00 , B32B15/00
CPC分类号： B23K26/30 , B23K1/0018 , B23K2101/001 , F01D9/023 , F23R3/005 , F23R3/42 , F23R2900/00017 , F23R2900/00018 , Y02T50/67 , Y02T50/675 , Y10T29/49826 , Y10T29/49893 , Y10T428/12493
摘要： A plate-like-object manufacturing method, plate-like objects, a gas-turbine combustor, and a gas turbine, in which degradation in the cooling performance can be suppressed, the time required for manufacturing a gas-turbine combustor can be shortened, and deterioration of the working environment can be prevented are provided. A plate-like-object manufacturing method includes a step of forming a plate-like object by stacking a plurality of plates and arranging a plurality of channels, through which a cooling medium flows, side-by-side between the plurality of plates; and a step of arranging a plurality of the plate-like objects side-by-side in a direction in which the channels are arranged, butting the plurality of plate-like objects against each other, and performing welding at an abutment section. The channels adjacent to the abutment section extend along the abutment section and have a greater dimension in the direction in which the channels are arranged, as compared with that of other channels.
摘要翻译：能够抑制冷却性能的劣化的板状物体，燃气轮机燃烧器和燃气轮机，能够缩短制造燃气轮机燃烧器所需的时间，并且可以防止工作环境的劣化。板状物体的制造方法包括通过堆叠多个板并且在多个板之间并排布置冷却介质流过的多个通道来形成板状物体的步骤; 以及在排列通道的方向并列配置多个板状物体的步骤，使多个板状物体彼此抵接，并在邻接部分进行焊接。与邻接部分相邻的通道相对于其它通道而言沿着邻接部分延伸并且在通道布置方向上具有更大的尺寸。

2. 发明授权

US08661827B2 Plates having cooling channels, and method for welding the plates and increasing a dimension of the cooling channels adjacent the welded section 有权
标题翻译：具有冷却通道的板，以及用于焊接板的方法和增加与焊接部分相邻的冷却通道的尺寸
公开(公告)号：US08661827B2
公开(公告)日：2014-03-04
申请号：US12646115
申请日：2009-12-23
申请人： Hitoshi Morimoto , Hidenori Kanki , Tatsuo Ishiguro , Hiroki Shibata , Tetsu Konishi , Kenji Sato
发明人： Hitoshi Morimoto , Hidenori Kanki , Tatsuo Ishiguro , Hiroki Shibata , Tetsu Konishi , Kenji Sato
IPC分类号： F02C1/00
CPC分类号： B23K26/30 , B23K1/0018 , B23K2101/001 , F01D9/023 , F23R3/005 , F23R3/42 , F23R2900/00017 , F23R2900/00018 , Y02T50/67 , Y02T50/675 , Y10T29/49826 , Y10T29/49893 , Y10T428/12493
摘要： A plate-like-object manufacturing method, plate-like objects, a gas-turbine combustor, and a gas turbine, in which degradation in the cooling performance can be suppressed, the time required for manufacturing a gas-turbine combustor can be shortened, and deterioration of the working environment can be prevented are provided. A plate-like-object manufacturing method includes a step of forming a plate-like object by stacking a plurality of plates and arranging a plurality of channels, through which a cooling medium flows, side-by-side between the plurality of plates; and a step of arranging a plurality of the plate-like objects side-by-side in a direction in which the channels are arranged, butting the plurality of plate-like objects against each other, and performing welding at an abutment section. The channels adjacent to the abutment section extend along the abutment section and have a greater dimension in the direction in which the channels are arranged, as compared with that of other channels.
摘要翻译：能够抑制冷却性能的劣化的板状物体，燃气轮机燃烧器和燃气轮机，能够缩短制造燃气轮机燃烧器所需的时间，并且可以防止工作环境的劣化。板状物体的制造方法包括通过堆叠多个板并且在多个板之间并排布置冷却介质流过的多个通道来形成板状物体的步骤; 以及在排列通道的方向并列配置多个板状物体的步骤，使多个板状物体彼此抵接，并在邻接部分进行焊接。与邻接部分相邻的通道相对于其它通道而言沿着邻接部分延伸并且在通道布置方向上具有更大的尺寸。

3. 发明申请

US20090260342A1 GAS TURBINE 审中-公开
标题翻译：燃气轮机
公开(公告)号：US20090260342A1
公开(公告)日：2009-10-22
申请号：US12442141
申请日：2007-09-04
申请人： Tatsuo Ishiguro , Katsunori Tanaka , Tetsu Konishi
发明人： Tatsuo Ishiguro , Katsunori Tanaka , Tetsu Konishi
IPC分类号： F02C7/10 , F02C7/00
CPC分类号： F02C7/18 , F02C1/04 , F02C7/08 , F02C7/224 , F05D2260/205 , Y02E20/16
摘要： A gas turbine, in which compressed air that is compressed by a compressor (11) is mixed with fuel in a combustor (12), the mixture is burned to produce combustion gas, and the combustion gas is provided to a turbine (13) to produce rotative power, includes: a pressurizing unit (41) that pressurizes some of the compressed air that is compressed by the compressor (11); a combustor cooling unit (42) that cools the combustor (12) with the compressed air that is pressurized by the pressurizing unit (41); and a compressed air circulation line (46) that provides the compressed air to the casing of the combustor (12). In the gas turbine, the combustor can be cooled by minimizing pressure loss of the compressed air, and degradation of the power efficiency can be prevented.
摘要翻译：一种燃气轮机，其中由压缩机（11）压缩的压缩空气与燃料（12）中的燃料混合，燃烧所述混合物以产生燃烧气体，并且将燃烧气体提供给涡轮机（13）至产生旋转动力，包括：加压单元（41），其对由压缩机（11）压缩的一些压缩空气加压; 燃烧器冷却单元（42），其利用由加压单元（41）加压的压缩空气来冷却燃烧器（12）; 以及将压缩空气提供给燃烧器（12）的壳体的压缩空气循环管线（46）。在燃气轮机中，可以通过使压缩空气的压力损失最小化来冷却燃烧室，能够防止功率效率的劣化。

4. 发明授权

US09512781B2 Cooling structure for recovery-type air-cooled gas turbine combustor 有权
标题翻译：回收式风冷式燃气轮机燃烧器的冷却结构
公开(公告)号：US09512781B2
公开(公告)日：2016-12-06
申请号：US13806523
申请日：2011-08-10
申请人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Shunsuke Torii , Yuya Fukunaga , Tetsu Konishi , Yoshiaki Nishimura , Yoshiaki Igarashi , Shinya Ishikawa
发明人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Shunsuke Torii , Yuya Fukunaga , Tetsu Konishi , Yoshiaki Nishimura , Yoshiaki Igarashi , Shinya Ishikawa
IPC分类号： F02C7/12 , F02C6/08 , F02C7/18 , F01D9/02 , F02C7/08 , F02C7/24 , F23R3/00 , F23R3/06 , F23R3/44
CPC分类号： F02C7/18 , F01D9/023 , F02C7/08 , F02C7/24 , F05D2260/202 , F23R3/005 , F23R3/06 , F23R3/44 , F23R2900/00014
摘要： In a cooling structure for a recovery-type air-cooled gas turbine combustor having a recovery-type air-cooling structure that bleeds, upstream of the combustor, and pressurizes compressed air supplied from a compressor, that uses the bled and pressurized air to cool a wall, and that recovers and reuses the bled and pressurized air as combustion air for burning fuel in the combustor together with a main flow of the compressed air, wall cooling in which cooling air is supplied to cooling air passages formed in the wall of the combustor to perform cooling involves a downstream wall region, closer to a turbine, that is cooled using the bled and pressurized air as the cooling air and an upstream wall region, closer to a burner, that is cooled using, as the cooling air, bled compressed air bled from a main flow of the compressed air through a housing inner space.
摘要翻译：在用于具有回收式空气冷却结构的回收式空气冷却燃气轮机燃烧器的冷却结构中，所述回收型空气冷却结构在燃烧器的上游出来并对从压缩机供给的压缩空气进行加压，所述回收式空气冷却结构使用过滤和加压空气来冷却一个墙壁，并且回收和再利用排放和加压的空气作为用于燃烧燃烧器中的燃料的燃烧空气以及压缩空气的主流，壁冷却，其中冷却空气被供应到冷却空气通道用于进行冷却的燃烧器包括更靠近涡轮机的下游壁区域，其使用作为冷却空气的排放和加压空气以及更靠近燃烧器的上游壁区域冷却，所述上游壁区域作为冷却空气被排出压缩空气从压缩空气的主流流过壳体内部空间。

5. 发明申请

US20130098063A1 COOLNG STRUCTURE FOR RECOVERY-TYPE AIR-COOLED GAS TURBINE COMBUSTOR 有权
标题翻译：回收式空气冷却气涡轮机的冷却结构
公开(公告)号：US20130098063A1
公开(公告)日：2013-04-25
申请号：US13806523
申请日：2011-08-10
申请人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Shunsuke Torii , Yuya Fukunaga , Tetsu Konishi , Yoshiaki Nishimura , Yoshiaki Igarashi , Shinya Ishikawa
发明人： Satoshi Mizukami , Tatsuo Ishiguro , Junichiro Masada , Kazumasa Takata , Shunsuke Torii , Yuya Fukunaga , Tetsu Konishi , Yoshiaki Nishimura , Yoshiaki Igarashi , Shinya Ishikawa
IPC分类号： F02C7/18 , F23R3/06 , F02C7/08
CPC分类号： F02C7/18 , F01D9/023 , F02C7/08 , F02C7/24 , F05D2260/202 , F23R3/005 , F23R3/06 , F23R3/44 , F23R2900/00014
摘要： In a cooling structure for a recovery-type air-cooled gas turbine combustor having a recovery-type air-cooling structure that bleeds, upstream of the combustor, and pressurizes compressed air supplied from a compressor, that uses the bled and pressurized air to cool a wall, and that recovers and reuses the bled and pressurized air as combustion air for burning fuel in the combustor together with a main flow of the compressed air, wall cooling in which cooling air is supplied to cooling air passages formed in the wall of the combustor to perform cooling involves a downstream wall region, closer to a turbine, that is cooled using the bled and pressurized air as the cooling air and an upstream wall region, closer to a burner, that is cooled using, as the cooling air, bled compressed air bled from a main flow of the compressed air through a housing inner space.
摘要翻译：在用于具有回收式空气冷却结构的回收式空气冷却燃气轮机燃烧器的冷却结构中，所述回收型空气冷却结构在燃烧器的上游出来并对从压缩机供给的压缩空气进行加压，所述回收式空气冷却结构使用过滤和加压空气来冷却一个墙壁，并且回收和再利用排放和加压的空气作为用于燃烧燃烧器中的燃料的燃烧空气以及压缩空气的主流，壁冷却，其中冷却空气被供应到冷却空气通道用于进行冷却的燃烧器包括更靠近涡轮机的下游壁区域，其使用作为冷却空气的排放和加压空气以及更靠近燃烧器的上游壁区域冷却，所述上游壁区域作为冷却空气被流出压缩空气从压缩空气的主流流过壳体内部空间。

6. 发明授权

US07908866B2 Gas turbine combustor 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US07908866B2
公开(公告)日：2011-03-22
申请号：US11660268
申请日：2006-03-17
申请人： Eigo Kato , Mitsuru Kondo , Tatsuo Ishiguro , Masaki Ono , Tetsu Konishi , Tetsuya Iwamoto
发明人： Eigo Kato , Mitsuru Kondo , Tatsuo Ishiguro , Masaki Ono , Tetsu Konishi , Tetsuya Iwamoto
IPC分类号： F02C1/00 , F02G3/00
CPC分类号： F23R3/42 , F01D9/023 , F01D11/005 , F05D2230/642 , F23R3/60 , F23R2900/00005
摘要： An object of the present invention is to provide a gas turbine combustor with improved fatigue resistance of a combustor. It is possible to intentionally reduce a stiffness of each of flanges of upper and lower walls of an end portion (outlet) of the tail pipe of the gas turbine combustor. It is possible to reduce a stiff difference between the upper and lower walls of the end portion (outlet) of the tail pipe section and side walls. Thus, it is possible to reduce compulsion deformation caused due to thermal stress generated in the end portion (outlet) of the tail pipe section on the operation of the conventional gas turbine combustor, and to reduce high stress easy to generate in the side plate. As a result, the gas turbine combustor with high fatigue resistance can be realized.
摘要翻译：本发明的目的是提供一种具有改进的燃烧器的抗疲劳性的燃气轮机燃烧器。可以有意地降低燃气轮机燃烧器的尾管的端部（出口）的上壁和下壁的每个凸缘的刚度。可以减少尾管部分的端部（出口）和侧壁的上壁和下壁之间的刚性差。因此，能够减少由于在现有的燃气轮机燃烧器的运转时尾管部的端部（出口）产生的热应力引起的强制变形，并且能够降低侧板容易产生的高应力。结果，能够实现耐疲劳性高的燃气轮机燃烧器。

7. 发明申请

US20080010989A1 Gas Turbine Combustor 有权
标题翻译：燃气轮机燃烧器
公开(公告)号：US20080010989A1
公开(公告)日：2008-01-17
申请号：US11660268
申请日：2006-03-17
申请人： Eigo Kato , Mitsuru Kondo , Tatsuo Ishiguro , Masaki Ono , Tetsu Konishi , Tetsuya Iwamoto
发明人： Eigo Kato , Mitsuru Kondo , Tatsuo Ishiguro , Masaki Ono , Tetsu Konishi , Tetsuya Iwamoto
IPC分类号： F02C1/00
CPC分类号： F23R3/42 , F01D9/023 , F01D11/005 , F05D2230/642 , F23R3/60 , F23R2900/00005
摘要： An object of the present invention is to provide a gas turbine combustor with improved fatigue resistance of a combustor. It is possible to intentionally reduce a stiffness of each of flanges of upper and lower walls of an end portion (outlet) of the tail pipe of the gas turbine combustor. It is possible to reduce a stiff difference between the upper and lower walls of the end portion (outlet) of the tail pipe section and side walls. Thus, it is possible to reduce compulsion deformation caused due to thermal stress generated in the end portion (outlet) of the tail pipe section on the operation of the conventional gas turbine combustor, and to reduce high stress easy to generate in the side plate. As a result, the gas turbine combustor with high fatigue resistance can be realized.
摘要翻译：本发明的目的是提供一种具有改进的燃烧器的抗疲劳性的燃气轮机燃烧器。可以有意地降低燃气轮机燃烧器的尾管的端部（出口）的上壁和下壁的每个凸缘的刚度。可以减少尾管部分的端部（出口）和侧壁的上壁和下壁之间的刚性差。因此，能够减少由于在现有的燃气轮机燃烧器的运转时尾管部的端部（出口）产生的热应力引起的强制变形，并且能够降低侧板容易产生的高应力。结果，能够实现耐疲劳性高的燃气轮机燃烧器。

8. 发明授权

US08813502B2 Cooling structure of gas turbine combustor 有权
标题翻译：燃气轮机燃烧器的冷却结构
公开(公告)号：US08813502B2
公开(公告)日：2014-08-26
申请号：US12598100
申请日：2008-09-24
申请人： Tatsuo Ishiguro , Katsunori Tanaka , Kotaro Miyauchi
发明人： Tatsuo Ishiguro , Katsunori Tanaka , Kotaro Miyauchi
IPC分类号： F02C1/08 , F02G1/055 , F02C7/12 , F23R3/28 , F23R3/00 , F23R3/06
CPC分类号： F23R3/283 , F23R3/005 , F23R3/06 , F23R2900/03042 , F23R2900/03044
摘要： It is required for a gas turbine combustor to exhaust low NOx. The gas turbine combustor is provided with a combustion tube which has a cooling passage through which cooling air flows in a double wall structure. The cooling passage has a main cooling air supply opening opened to a side of a combustion zone. The cooling air supplied from the main cooling air supply opening is guided to a direction along an inner wall surface of the combustion tube by a guide. The cooling air flows through the cooling passage inside the combustion tube, and then is reused for film cooling along the inner wall surface. Thus, it is possible to save cooling air. Therefore, a more part of the air supplied from a compressor can be used as air for combustion and it becomes possible to exhaust low NOx.
摘要翻译：燃气轮机燃烧器需要排出低NOx。燃气轮机燃烧器设置有燃烧管，该燃烧管具有冷却空气以双壁结构流动的冷却通道。冷却通道具有向燃烧区侧面敞开的主冷却空气供给口。从主冷却空气供给口供给的冷却空气通过引导件被引导到燃烧管的内壁面的方向。冷却空气流过燃烧管内的冷却通道，然后再次用于沿内壁表面进行膜冷却。因此，可以节省冷却空气。因此，从压缩机供给的空气的一部分能够用作燃烧用空气，能够排出低NOx。

9. 发明授权

US08698342B2 Wind turbine generating apparatus 失效
标题翻译：风力发电机组
公开(公告)号：US08698342B2
公开(公告)日：2014-04-15
申请号：US13244383
申请日：2011-09-24
申请人： Shigeto Hirai , Shinsuke Sato , Tatsuo Ishiguro
发明人： Shigeto Hirai , Shinsuke Sato , Tatsuo Ishiguro
IPC分类号： F03D9/00 , F03D11/02
CPC分类号： F03D80/60 , F03D9/25 , F05B2240/14 , F05B2240/912 , F05B2260/2241 , F05B2260/64 , Y02E10/726 , Y02E10/728
摘要： A wind turbine generating apparatus includes a rotor head that rotates upon receiving outside wind on a wind turbine blade, a generator that generates electricity, and a nacelle interior air passage through which outside air flows isolatedly from an interior space of the nacelle.
摘要翻译：一种风力涡轮发电装置，包括：转子头，其在接收到风力涡轮机叶片上的外部风力时旋转;发电机，其产生电力;以及机舱内部空气通道，外部空气从所述机舱的内部空间隔离流动。

10. 发明申请

US20100180601A1 COOLING STRUCTURE OF GAS TURBINE COMBUSTOR 有权
标题翻译：燃气轮机组的冷却结构
公开(公告)号：US20100180601A1
公开(公告)日：2010-07-22
申请号：US12598100
申请日：2008-09-24
申请人： Tatsuo Ishiguro , Katsunori Tanaka , Kotaro Miyauchi
发明人： Tatsuo Ishiguro , Katsunori Tanaka , Kotaro Miyauchi
IPC分类号： F02C3/14
CPC分类号： F23R3/283 , F23R3/005 , F23R3/06 , F23R2900/03042 , F23R2900/03044
摘要： It is required for a gas turbine combustor to exhaust low NOx. The gas turbine combustor is provided with a combustion tube which has a cooling passage through which cooling air flows in a double wall structure. The cooling passage has a main cooling air supply opening opened to a side of a combustion zone. The cooling air supplied from the main cooling air supply opening is guided to a direction along an inner wall surface of the combustion tube by a guide. The cooling air flows through the cooling passage inside the combustion tube, and then is reused for film cooling along the inner wall surface. Thus, it is possible to save cooling air. Therefore, a more part of the air supplied from a compressor can be used as air for combustion and it becomes possible to exhaust low NOx.
摘要翻译：燃气轮机燃烧器需要排出低NOx。燃气轮机燃烧器设置有燃烧管，该燃烧管具有冷却空气以双壁结构流动的冷却通道。冷却通道具有向燃烧区侧面敞开的主冷却空气供给口。从主冷却空气供给口供给的冷却空气通过引导件被引导到燃烧管的内壁面的方向。冷却空气流过燃烧管内的冷却通道，然后再次用于沿内壁表面进行膜冷却。因此，可以节省冷却空气。因此，从压缩机供给的空气的一部分能够用作燃烧用空气，能够排出低NOx。

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